Garmin G1000 - Diamond DA42NG User guide

®

G1000

®

Pilot’s Guide

G1000

®

Integrated Flight Deck

Pilot’s Guide

Diamond DA42NG

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

Tel: 913.397.8200

Fax: 913.397.8282

AOG Hotline: 913.397.0836

Aviation Dealer

Technical Support: 888.606.5482

www.garmin.com

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax: 503.364.2138

Garmin (Europe) Ltd.

Liberty House,Houndsdown Business Park

Southampton, Hampshire, SO40 9LR, U.K.

Tel: +44 (0) 238 052 4000

Fax: +44 (0) 238 052 4004

Aviation Support: +44 (0) 370 850 1243

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District,

New Taipei City, Taiwan

Tel: 34-93-357-2608

Fax: 34-93-429-4484

Diamond DA42NG

190-00962-04

Revision A

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. A

This manual reﬂects the operation of System Software version 0752.13 or later for the Diamond DA42NG Some differences in operation

may be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

Tel: 913.397.8200

Fax: 913.397.8282

Aircraft On Ground (AOG) Hotline: 913.397.0836

Aviation Dealer Technical Support: 888.606.5482

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Tel: 44.(0).23.8052.4000

Fax: 44.(0).23.8052.4004

Aviation Support: 44.(0).37.0850.1243

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax 503.364.2138

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Tel: 34.93.357.2608

Fax: 34.93.429.4484

Website Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored

in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download

a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for

personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice

and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000

®

is a trademark of Garmin Ltd. or its subsidiaries. These

trademarks may not be used without the express permission of Garmin.

Honeywell

®

is a registered trademark of Honeywell International, Inc. Stormscope

®

is a registered trademark of L-3 Communications.

Avidyne

®

is a registered trademark of Avidyne Corporation. AC-U-KWIK

®

is a registered trademark of Penton Business Media Inc. SiriusXM

Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,

with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties

of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any

representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any

incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if

AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to

the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual

or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for

incidental or consequential damages so the above limitations or exclusions may not apply to you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with

respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of

merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or

make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the

maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related

to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions

do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations

or exclusions may not apply to licensee.

May 2016 Printed in the U.S.A

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

i

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation

from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot

independently verify the accuracy of the information.

WARNING: Always refer to current aeronautical charts and NOTAMs for veriﬁcation of displayed aeronautical

information. Displayed aeronautical data may not incorporate the latest NOTAM information.

WARNING: Do not use geometric altitude for compliance with air trafﬁc control altitude requirements. The

primary barometric altimeter must be used for compliance with all air trafﬁc control altitude regulations,

requirements, instructions, and clearances.

WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap

data is intended only to supplement other approved navigation data sources and should be considered only

an aid to enhance situational awareness.

WARNING: Do not rely solely upon the display of trafﬁc information to accurately depict all of the trafﬁc

within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information

from aircraft or ground stations, trafﬁc may be present that is not represented on the display.

WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous

weather. Information contained within data link weather products may not accurately depict current

weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather

information shown by the data link weather product. Due to time delays inherent in gathering and processing

weather data for data link transmission, the weather information shown by the data link weather product

may be signiﬁcantly older than the indicated weather product age.

WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied

upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical

charts for appropriate minimum clearance altitudes.

WARNING: Always obtain qualiﬁed instruction prior to operational use of this equipment.

WARNING

:

Do not use a QFE altimeter setting with this system. System functions will not operate properly

with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the

standard pressure setting, as applicable.

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Aii

WARNINGS, CAUTIONS, AND NOTES

WARNING

:

Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

WARNING: When using the autopilot to ﬂy an approach with vertical guidance, the autopilot will not level

the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.

WARNING: Do not rely solely upon the display of trafﬁc information for collision avoidance maneuvering.

The trafﬁc display does not provide collision avoidance resolution advisories and does not under any

circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, do not rely on the accuracy of attitude and

heading indications (GRS 77 installations only) in the following geographic areas: North of 72° North

latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between

longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and

128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern

Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and

New Zealand).

WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous

weather avoidance. Range limitations and interference may cause the system to display inaccurate or

incomplete information. Refer to documentation from the lightning detection system manufacturer for

detailed information about the system.

WARNING:

Use appropriate primary systems for navigation, and for terrain, obstacle, and trafﬁc avoidance.

Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or

reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or trafﬁc.

WARNING:

Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may

appear as a partial symbol.

WARNING:

Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of

the aircraft to the runway or for maintaining the proper approach path angle during landing.

WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within

the MPEL boundary.

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

iii

WARNINGS, CAUTIONS, AND NOTES

WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of

precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color

not representative of the true intensity.

CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will

harm the anti-reﬂective coating.

CAUTION:

Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or

modiﬁcations could void both the warranty and affect the airworthiness of the aircraft.

NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.

Always conﬁrm TFR information through ofﬁcial sources such as Flight Service Stations or Air Trafﬁc Control.

NOTE: All visual depictions contained within this document, including screen images of the system panel

and displays, are subject to change and may not reﬂect the most current system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

NOTE: The United States government operates the Global Positioning System and is solely responsible for

its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and

performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation

AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or

misinterpreted and, therefore, become unsafe.

NOTE

: This device complies with part 15 of the FCC Rules. Operation is subject to the following two

conditions: (1) this device may not cause harmful interference, and (2) this device must accept any

interference received, including interference that may cause undesired operation.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE

: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic ﬁelds

can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut

down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no

comparison is possible.

NOTE: The system responds to a terminal procedure based on data coded within that procedure in the

Navigation Database. Differences in system operation may be observed among similar types of procedures

due to differences in the Navigation Database coding speciﬁc to each procedure.

NOTE

: The FAA has asked Garmin to remind pilots who ﬂy with Garmin database-dependent avionics of the

following:

• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information

related to the use of databases in the National Airspace System.

• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases

obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue

of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database

and can be viewed at http://ﬂy.garmin.com by selecting ‘Type 2 LOA Status.’

• Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with

established FAA regulatory guidance, but does not constitute authorization to ﬂy any and all terminal procedures

that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established

AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE

: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in

SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at

www.ﬂygarmin.com by selecting ‘Database Exclusions List.’

NOTE

: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their

impact on the intended aircraft operation. The database alerts can be viewed at www.ﬂygarmin.com by

selecting ‘Aviation Database Alerts.’

NOTE

: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to

coordinate the revised DQRs.

NOTE: Garmin requests the ﬂight crew report any observed discrepancies related to database information.

These discrepancies could come in the form of an incorrect procedure; incorrectly identiﬁed terrain, obstacles

and ﬁxes; or any other displayed item used for navigation or communication in the air or on the ground. Go

to FlyGarmin.com and select ‘Aviation Data Error Report’.

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

v

WARNINGS, CAUTIONS, AND NOTES

NOTE: Lamp(s) inside this product contain mercury (HG) and must be recycled or disposed of according to

local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/

environment/disposal.jsp

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms

that can cause isolated discharge points in the strike display mode. However, clusters of two or more

discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after

the screen has been cleared.

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Avi

WARNINGS, CAUTIONS, AND NOTES

Blank Page

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

vii

REVISION INFORMATION

Record of Revision

Part Number Revision Date Page Range Description

190-00962-00 A 02/19/09 i – I-6 Initial release with GDU SW Version 9.05

190-00962-00 B 04/29/09 i – I-6 Added Synthetic Vision System

190-00962-01 A 03/14/11 i – I-6 Added GDU 11.12

Added Database Synchronization

Added Electronic Checklists

Added AOPA Airport Directory

Added ﬂight plan import/export

Added Auxiliary Video

Changed procedure for creating user waypoints

190-00962-02 A 06/15/12 i – I-6 Added GDU 12.03

190-00962-02 B March

2014

All Added Underspeed Protection

Updated ESP pitch limits

Changed GFC 700 to Garmin AFCS

Added LP approaches

190-00962-03 A October

2014

All Updated System Message Advisories

Updated Weather Radar

Added Radar Altimeter

Updated EIS strip

Added ADS-B out capablility

Added other GDU 14.02 parameters

Changed GFDS to Connext

Changed Synthetic Vision System (SVS) to Synthetic Vision

Technology (SVT)

Added User Deﬁned Holding Patterns

Added Temperature Compensated Altitude

Updated Warnings, Cautions, and Notes

190-00962-04 A May 2016 All Added Support for GDL 69/69A SXM

Added Support for ADS-B Trafﬁc

Added Support for FIS-B Weather

Added Bluetooth

®

connectivity

Updated Warnings, Cautions, and Notes

Added other GDU 15.11 parameters

Added Support for GSR 56 Iridium Transceiver

Added Wi-Fi connectivity

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Aviii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 Line Replaceable Units ........................................... 2

1.2 Secure Digital (SD) Cards .......................................6

1.3 System Power-up ..................................................... 7

1.4 System Operation .................................................... 8

Display Operation ......................................................... 8

G1000 System Annunciations ........................................ 9

System Status ............................................................. 11

AHRS Operation ......................................................... 13

GPS Receiver Operation .............................................. 14

1.5 G1000 Controls ...................................................... 18

PFD/MFD Controls ...................................................... 18

Softkey Function ......................................................... 20

1.6 Accessing G1000 Functionality............................ 27

Menus ....................................................................... 27

Data Entry.................................................................. 27

Page Groups .............................................................. 29

System Settings .......................................................... 34

Timers ....................................................................... 40

Electronic Checklists ................................................... 42

1.7 Display Backlighting ............................................. 45

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 50

Airspeed Indicator ...................................................... 50

Attitude Indicator ....................................................... 52

Altimeter ................................................................... 53

Vertical Speed Indicator (VSI) ....................................... 55

Vertical Deviation ....................................................... 56

Horizontal Situation Indicator (HSI) .............................. 57

Course Deviation Indicator (CDI) .................................. 62

2.2 Supplemental Flight Data .................................... 69

Outside Air Temperature .............................................. 69

Wind Data ................................................................. 71

Vertical Navigation (VNV) Indications ........................... 72

2.3 PFD Annunciations and Alerting Functions ........ 73

System Alerting .......................................................... 73

Marker Beacon Annunciations...................................... 74

Trafﬁc Annunciation .................................................... 74

Altitude Alerting ......................................................... 75

Low Altitude Annunciation .......................................... 75

Minimum Descent Altitude/Decision Height Alerting ...... 76

Radar Altimeter .......................................................... 77

2.4 Abnormal Operations ........................................... 79

Abnormal GPS Conditions ........................................... 79

Unusual Attitudes ....................................................... 80

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Display ....................................................... 84

3.2 System Display ...................................................... 86

3.3 Fuel Display ............................................................ 88

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 91

MFD/PFD Controls and Frequency Display ..................... 92

Audio Panel Controls .................................................. 94

4.2 COM Operation ...................................................... 96

COM Transceiver Selection and Activation ..................... 96

COM Transceiver Manual Tuning .................................. 97

Quick-tuning and Activating 121.500 MHz .................... 98

Auto-tuning the COM Frequency .................................. 99

Frequency Spacing .................................................... 103

Automatic Squelch .................................................... 104

Volume .................................................................... 104

4.3 NAV Operation ..................................................... 105

NAV Radio Selection and Activation ........................... 105

NAV Receiver Manual Tuning ..................................... 106

Auto-tuning a NAV Frequency from the MFD ............... 108

Marker Beacon Receiver ............................................ 113

ADF/DME Tuning ...................................................... 114

4.4 GTX 33 Mode S Transponder .............................. 118

Transponder Controls ................................................ 118

Transponder Mode Selection ...................................... 119

Entering a Transponder Code ..................................... 121

IDENT Function ........................................................ 122

ADS-B TX ................................................................. 123

Flight ID Reporting.................................................... 124

4.5 Additional Audio Panel Functions ..................... 125

Power-up ................................................................. 125

Mono/Stereo Headsets .............................................. 125

Speaker ................................................................... 125

Intercom .................................................................. 126

Clearance Recorder and Player ................................... 128

Split COM ................................................................ 129

Entertainment Inputs ................................................ 129

4.6 Audio Panel Preﬂight Procedure ....................... 130

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Garmin G1000 Pilot’s Guide for the Diamond DA42NG

ix

TABLE OF CONTENTS

4.7 Abnormal Operation ........................................... 131

Stuck Microphone ..................................................... 131

COM Tuning Failure ................................................... 131

Audio Panel Fail-Safe Operation ................................. 131

Reversionary Mode ................................................... 131

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 133

Navigation Status Box ............................................... 134

5.2 Using Map Displays ............................................. 136

Map Orientation ....................................................... 136

Map Range .............................................................. 138

Map Panning ............................................................ 140

Measuring Bearing and Distance ................................ 145

Topography .............................................................. 146

Map Symbols ........................................................... 149

Airways ................................................................... 155

Track Vector ............................................................. 157

Wind Vector ............................................................. 158

Nav Range Ring........................................................ 159

Fuel Range Ring ....................................................... 160

Field of View (SVS) .................................................... 161

Selected Altitude Intercept Arc ................................... 162

5.3 Waypoints ............................................................. 163

Airports ................................................................... 164

Intersections ............................................................ 171

NDBs ....................................................................... 173

VORs ....................................................................... 175

VRPs ....................................................................... 177

User Waypoints ........................................................ 179

5.4 Airspaces .............................................................. 185

5.5 Direct-to-Navigation .......................................... 189

5.6 Flight Planning ..................................................... 194

Flight Plan Creation .................................................. 195

Adding Waypoints to an Existing Flight Plan ................ 202

Adding Airways to a Flight Plan ................................. 205

Adding Procedures to a Stored Flight Plan .................. 207

Flight Plan Storage ................................................... 214

Flight Plan Editing .................................................... 216

Along Track Offsets ................................................... 219

Parallel Track ............................................................ 221

Activating a Flight Plan Leg ....................................... 224

Inverting a Flight Plan ............................................... 225

Flight Plan Views ...................................................... 226

Closest Point of FPL .................................................. 228

User-Deﬁned Holding Patterns ................................... 228

5.7 Vertical Navigation ............................................. 233

Altitude Constraints .................................................. 235

5.8 Procedures ...........................................................239

Departures ............................................................... 240

Arrivals ................................................................... 243

Approaches ............................................................. 246

5.9 Trip Planning ........................................................ 254

Trip Planning ............................................................ 254

5.10 RAIM Prediction................................................... 258

5.11 Navigating a Flight Plan ..................................... 261

5.12 Abnormal Operation ........................................... 289

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 292

Activating Services .................................................... 292

Using SiriusXM Weather Products .............................. 293

6.2 Garmin Connext Weather ................................... 326

Registering the Iridium Satellite System ...................... 326

Registering Garmin Connext Weather ......................... 327

Accessing Garmin Connext Weather Products .............. 329

Connext Data Requests ............................................. 336

Garmin Connext Weather Products ............................. 340

Abnormal Operations ................................................ 355

6.3 FIS-B Weather ...................................................... 357

Using FIS-B Weather Products .................................... 357

FIS-B Weather Status................................................. 379

6.4 Airborne Color Weather Radar .......................... 380

System Description ................................................... 380

Principles of Pulsed Airborne Weather Radar ............... 380

Safe Operating Distance ............................................ 384

Basic Antenna Tilt Setup ............................................ 385

Weather Mapping and Interpretation ......................... 386

Ground Mapping and Interpretation ........................... 396

Weather Radar Overlay on the Navigation Map Page ... 397

System Status ........................................................... 399

6.5 WX-500 Stormscope ........................................... 401

Setting Up Stormscope on the Navigation Map ........... 401

Selecting the Stormscope Page .................................. 405

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Ax

TABLE OF CONTENTS

6.6 Terrain Proximity ................................................. 406

Displaying Terrain Proximity Data ............................... 406

Terrain Proximity Page ............................................... 409

6.7 Proﬁle View Terrain ............................................. 411

Proﬁle View Display .................................................. 412

6.8 Terrain-SVS ........................................................... 415

Displaying Terrain-SVS Data ....................................... 416

Terrain-SVS Page ...................................................... 418

Terrain-SVS Alerts ..................................................... 420

System Status ........................................................... 423

6.9 Trafﬁc Information Service (TIS) ........................ 424

Displaying Trafﬁc Data .............................................. 425

Trafﬁc Map Page ....................................................... 427

TIS Alerts ................................................................. 428

System Status ........................................................... 429

6.10 Avidyne TAS600 Trafﬁc ........................................ 432

TAS Symbology ......................................................... 432

Displaying Trafﬁc Data .............................................. 433

Altitude Display ........................................................ 435

Trafﬁc Map Page Display Range ................................. 435

TAS Alerts ................................................................ 437

System Status ........................................................... 438

6.11 Garmin GDL 88 ADS-B Trafﬁc ............................. 439

ADS-B System Overview ............................................ 439

ADS-B with TAS ........................................................ 441

Conﬂict Situational Awareness & Alerting ................... 441

Airborne and Surface Applications .............................. 444

Trafﬁc Description ..................................................... 445

Operation ................................................................ 445

System Status ........................................................... 454

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Controls ...................................................... 458

7.2 Flight Director Operation ................................... 460

Activating the Flight Director ..................................... 460

AFCS Status Box ....................................................... 461

Command Bars ......................................................... 462

Flight Director Modes ................................................ 462

7.3 Vertical Modes ..................................................... 463

Pitch Hold Mode (PIT) ............................................... 464

Selected Altitude Capture Mode (ALTS) ....................... 465

Altitude Hold Mode (ALT) .......................................... 466

Vertical Speed Mode (VS) .......................................... 467

Flight Level Change Mode (FLC) ................................. 468

Vertical Navigation Modes (VPTH, ALTV) ..................... 469

Glidepath Mode (GP) (SBAS only) ............................... 474

Glideslope Mode (GS) ............................................... 476

Go Around Mode (GA) .............................................. 477

7.4 Lateral Modes ...................................................... 478

Roll Hold Mode (ROL) ............................................... 479

Heading Select Mode (HDG) ...................................... 480

Navigation Modes (GPS, VOR, LOC, BC) ...................... 481

Approach Modes (GPS, VAPP, LOC) ............................. 483

7.5 Autopilot and Yaw Damper Operation ............. 485

Flight Control ........................................................... 485

Engaging the Autopilot and Yaw Damper .................... 486

Control Wheel Steering ............................................. 486

Disengaging the Autopilot and Yaw Damper ................ 487

7.6 Example Flight Plan ............................................ 488

Departure ................................................................ 488

Intercepting a VOR Radial .......................................... 490

Flying a Flight Plan/GPS Course ................................. 491

Descent ................................................................... 492

Approach ................................................................. 495

Go Around/Missed Approach ..................................... 498

7.7 AFCS Annunciations and Alerts ......................... 500

AFCS Status Alerts .................................................... 500

Overspeed Protection ................................................ 501

Underspeed Protection .............................................. 501

Annunciations for KAP 140 Autopilot System .............. 503

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT) ..................... 507

SVT Operation .......................................................... 508

SVT Features ............................................................ 510

Field of View ............................................................ 519

8.2 SafeTaxi ................................................................ 521

8.3 ChartView ............................................................. 527

ChartView Softkeys ................................................... 528

Terminal Procedures Charts ....................................... 529

Chart Options ........................................................... 537

Day/Night View ........................................................ 543

ChartView Cycle Number and Expiration Date ............. 546

8.4 FliteCharts ............................................................ 549

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TABLE OF CONTENTS

FliteCharts Softkeys .................................................. 550

Terminal Procedures Charts ....................................... 551

Chart Options ........................................................... 558

Day/Night View ........................................................ 562

FliteCharts Cycle Number and Expiration Date ............. 564

8.5 Airport Directory ................................................. 569

Airport Directory Database Cycle Number and Revision 569

8.6 SiriusXM Satellite Radio Entertainment ........... 573

Activating SiriusXM Satellite Radio Services ................ 573

Using SiriusXM Radio ................................................ 575

8.7 Satellite Telephone Services .............................. 579

Telephone Communication ........................................ 579

Text Messaging (SMS) ............................................... 586

8.8 Electronic Stability and Protection (ESP

™

) ....... 599

Roll Engagement ...................................................... 600

Pitch Engagement..................................................... 601

High Airspeed Protection ........................................... 602

8.9 Scheduler .............................................................. 603

8.10 Electronic Checklists ........................................... 605

8.11 Flight Data Logging ............................................ 609

8.12 Auxiliary Video ..................................................... 611

Video Setup .............................................................612

Display Selection ...................................................... 612

Zoom/Range ............................................................ 614

8.13 WI-FI Connections ............................................... 615

8.14 Abnormal Operation ........................................... 621

SVT Troubleshooting ................................................. 621

Reversionary Mode ................................................... 621

Unusual Attitudes ..................................................... 622

GDL 69/69A Data Link Receiver Troubleshooting .......... 622

APPENDICES

Annunciations and Alerts ............................................. 625

Flight Plan Import/Export Messages ........................... 645

TAS Alerts and Annunciations .................................... 647

TIS Alerts and Annunciations...................................... 648

SVS Terrain Alerts ...................................................... 649

SVS Terrain Status Annunciations ............................... 649

ADS-B Alerts and Annunciations ................................. 650

Weather Radar Alerts and Annunciations .................... 651

GDL 69A/GDL 69A SXM Data Link Receiver Messages .. 652

Database Management ............................................. 653

Navigation Databases ............................................... 653

Garmin Databases/Jeppesen Chartview Database ........ 658

Magnetic Field Variation Database Update .................. 664

Garmin Aviation Glossary ............................................ 665

Frequently Asked Questions ........................................ 674

General TIS Information ............................................... 678

Introduction ............................................................. 678

TIS VS. TAS/TCAS ....................................................... 678

TIS Limitations.......................................................... 678

Map Symbols ................................................................. 680

Telephone/Text Messaging ......................................... 684

INDEX

Index ................................................................................ I-1

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. Axii

TABLE OF CONTENTS

Blank Page

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

1

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

SECTION 1 SYSTEM OVERVIEW

NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.

The G1000 Integrated Flight Deck System presents ﬂight instrumentation, position, navigation, communication,

and identiﬁcation information using ﬂat-panel color displays. The system is distributed across the following Line

Replaceable Units (LRUs):

•

GDU 1040

Primary Flight Display (PFD)

•

GDU 1045

Multi Function Display (MFD)

•

GMA 1347

Audio Panel with Integrated Marker

Beacon Receiver

•

GIA 63W

Integrated Avionics Units (IAU)

•

GDC 74A

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GTX 33 ES

Extended Squitter Mode S Transponder

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GDL 69/69A

or

69/69A SXM

Data Link Receiver

•

GSA 80

AFCS Yaw Damper Servo

•

GSA 81

AFCS Servos (3)

•

GSM 85 (

or

GSM 86)

Servo Mounts (4)

•

GSR 56

Iridium Transceiver

•

GWX 68/70

Weather Radar

•

GRA 5500

Radar Altimeter

•

Flight Stream 210

Wireless Bluetooth

®

Gateway

•

GDL 88

ADS-B Transceiver

•

GDL 59

Data Link

Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.

The Diamond DA42NG may be optionally equipped with a Garmin AFCS Automated Flight Control System,

providing ﬂight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. A2

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.1 LINE REPLACEABLE UNITS

• GDU 1040/1045 (2) – A GDU 1040 is conﬁgured as the Primary Flight Display (PFD) and a GDU 1045 as

the Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution.

The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each

display is also paired with an Ethernet connection to an IAU.

•

GMA 1347

– The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom,

and marker beacon controls, and is installed between the displays. This unit also provides manual control

of display Reversionary Mode (red

DISPLAY BACKUP

button; see Section 1.4, System Operation) and

communicates with both IAUs using an RS-232 digital interface.

•

GIA 63W

(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all LRUs

with the PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a ﬂight director (FD;

if Garmin AFCS is installed), and system integration microprocessors. Each GIA 63W is paired with the on-side

display via an HSDB connection. The IAUs are not paired together and do not communicate with each other

directly.

NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved.

•

GDC 74A

– The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature

(OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000

System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.

•

GEA 71

– The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This

unit communicates with both IAUs using an RS-485 digital interface.

•

GTX 33 or GTX 33 with Extended Squitter

– The GTX 33 solid-state Transponder provides Modes A, C, and

S capability. The GTX 33 with Extended Squitter will also provide 1090 MHz Extended Squitter (1090ES)

transmit capability. The transponder communicates with both IAUs through an RS-232 digital interface.

•

GRS 77

(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading

information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors

(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic ﬁeld

information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation

is discussed in Section 1.4, System Operation.

•

GMU 44

– The Magnetometer measures local magnetic ﬁeld and sends data to the AHRS for processing to

determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with

it via an RS-485 digital interface.

•

GDL 69/69A

or

69/69A SXM

– The Data Link Satellite Radio Receiver provides real-time weather information to

MFD maps and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment.

The Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite

Radio Service is required to enable Data Link Receiver capability.

•

GSA 80, GSA 81

and

GSM 85 (

or

GSM 86)

– The GSA servos are used for the automatic control of pitch, pitch

trim, roll and yaw. These units interface with each IAU.

The GSM 85 (or GSM 86) servo mounts are responsible for transferring the output torque of the servo actuators

to the mechanical ﬂight-control surface linkages (not displayed in Figure 1-1).

190-00962-04 Rev. A

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

3

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GRA 5500 (optional)

– The Radar Altimeter provides altitude above the ground (AGL) to the MFD, through the

GIA 63W, using an RS-422 digital interface.

•

GWX 68/70

– Provides airborne weather and ground mapped radar data to the MFD, via HSDB ethernet

connection.

•

GDL 88

(optional) – Provides ADS-B Trafﬁc in and FIS-B Weather.

•

Flight Stream 210

(optional) – Provides wireless Bluetooth connectivity between a compatible tablet/mobile

device and the avionics system.

•

GDL 59

(optional) – Provides Wi-Fi capability

•

GSR 56

(optional) – The Iridium Transceiver provides voice communication by means of pilot and copilot

headsets. The unit can also send and receive data over the Iridium satellite network.

Garmin G1000 Pilot’s Guide for the Diamond DA42NG

190-00962-04 Rev. A4

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

Figure 1-1 G1000 System Block Diagram

GMU 44

Magnetometer

Heading

Reversionary

Control

Reversionary

Control

GMA 1347

Audio Panel

GDU 1040

Primary Flight Display

GDU 1045

Multi Function Display

GDC 74A

Air Data

Computer

OAT

Airspeed

Altitude

Vertical Speed

GRS 77

AHRS

Attitude

Rate of Tu rn

Slip/Skid

GTX 33/33ES

Transponder

GEA 71

Engine/Airframe

Unit

GSA 81

Roll Servo

Autopilot Calculations

(optional)

GSA 81

Pitch Servo

Autopilot Calculations

(optional)

GSA 80

Ya w Damper Servo

Ya w Damper Calculations

(optional)

GSA 81

Pitch Tr im Servo

Autopilot Calculations

(optional)

No. 1 GIA 63W

Integrated Avionics Unit

System Inegration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS/SBAS

Glideslope

Flight Director (with AFCS option)

GPS Output

No. 2 GIA 63W

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS/SBAS

Glideslope

GPS Output

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